CA1169783A - Configuration for a disk brake torque tube assembly having replaceable keys and backplate - Google Patents

Configuration for a disk brake torque tube assembly having replaceable keys and backplate

Info

Publication number
CA1169783A
CA1169783A CA000399624A CA399624A CA1169783A CA 1169783 A CA1169783 A CA 1169783A CA 000399624 A CA000399624 A CA 000399624A CA 399624 A CA399624 A CA 399624A CA 1169783 A CA1169783 A CA 1169783A
Authority
CA
Canada
Prior art keywords
brake
torque tube
tube
key
inboard
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA000399624A
Other languages
French (fr)
Inventor
Harold E. Correll
Richard L. Crossman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Goodyear Aerospace Corp
Original Assignee
Goodyear Aerospace Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Goodyear Aerospace Corp filed Critical Goodyear Aerospace Corp
Application granted granted Critical
Publication of CA1169783A publication Critical patent/CA1169783A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D55/00Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes
    • F16D55/24Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes with a plurality of axially-movable discs, lamellae, or pads, pressed from one side towards an axially-located member
    • F16D55/26Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes with a plurality of axially-movable discs, lamellae, or pads, pressed from one side towards an axially-located member without self-tightening action
    • F16D55/36Brakes with a plurality of rotating discs all lying side by side
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D55/00Brakes with substantially-radial braking surfaces pressed together in axial direction, e.g. disc brakes
    • F16D2055/0004Parts or details of disc brakes
    • F16D2055/0058Fully lined, i.e. braking surface extending over the entire disc circumference
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/70Interfitted members
    • Y10T403/7018Interfitted members including separably interposed key
    • Y10T403/7021Axially extending
    • Y10T403/7024Longitudinally stepped or tapered

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Braking Arrangements (AREA)

Abstract

CONFIGURATION FOR A DISK BRAKE TORQUE TUBE
ASSEMBLY HAVING REPLACEABLE KEYS AND BACKPLATE
ABSTRACT OF THE DISCLOSURE
A unique configuration for a torque tube assembly (100) associated with a disk type brake comprises separable and replaceable keys (60) and a separable and replaceable brake disk backplate (70), The keys (60) are mounted in anti-rotation slots (52,54) at the inboard and outboard ends of the torque tube (50) and bolted to the barrel portion of the torque tube and are characterized by a radial extension (60d) that supports the separable back-plate (70). The torque tube (50) is a formed wrought metal tube that is mounted to the stationary portion of the brake housing (14) via bolts (69) that thread into the inboard end (60a) of the keys (60). In this configuration, the occurence of a defective key and/or backplate does not re-quire replacement of the total torque tube assembly.

Description

1 16~3 CONFIGUR~TION FOR A DISK BRAKE TORQUE TUBE
ASSEMBLY HAVING REPLACEABLE KEYS AND BACKPLATE
BACKGROUND OF T~ INVENTION
; This invention generally pertains to disk brakes and more particularly to a unique configuration for a torque - tube, drive key, and backplate assembly which may be applied to various type disk brake applications. More speci~`ically, the invention provides a torque tube having separable and replaceable keys and a separable and re-placeable backplate. While the invention will be described herein with regard to aircraft wheel and brake configura-tions, it may as well be applied to other type vehicle disk brakc configurations and various industrial brake applications. The invention therefore, is not considered limited in scope by the specific application illustrated in the drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
Various features and advantages of the invention will be better understood and appreciated from a consid-eration of the following detailed description of the pre-ferred embodiment when taken in conjunction with the accompanying drawings in the several figures in which like parts bear like reference numerals and in which:
FIGURE 1 is a sectional elevational view of a portion of a conventional prior art aircraft wheel and brake assembly, the portions that are pertinent to this inven-tion bein~ shown in solid lines while the non-pertinent portions are shown in ghost lines;
FIGURE 2 is an elevational view, in section, of a portion ol` a torque tube assembly in accordance with this invention;
FIGURE 3 is a partial sectional view as may be taken on line 3-3 of FIGURE 2;
FIGURE 4 is an elevational view of the inboard end showing a portion of the torque tube assembly as may be taken on line 4-4 of FIGIJRE 2; and FIGURE 5 is an elevational view of the outboard end showin~ a portion of the torque tube assembly as may bo taken Oll line 5-5 of FIGURE 2.
J- ~

1 1~9783 lA
'.
By way o~ example, FIGURE 1 of the drawings is illustrativc o~' a conventional prior art aircraft wheel and brake assembly generally indicated by reference numcral 10. Portions which are pertinent to the invention are indicated in solid lines while less pertinent portions arc indicated via ghost lines for the purpose of illu-strating the environment thereof. Very generally, a wheel and brake assembly 10 may include a two-part wheel 12 comprised of an inboard wheel half 12a and an outboard wheel half 12b which are fastened together by a plurality of wheel bolts 12c and mounted for rotation about an axle 14 via a plurality of wheel bearings diagramatically indi-cated at 16. A multi-disk brake assembly generally indi-cated by refercncc numeral 20 may be mounted at the in-board side of the wheel 12 within the wheel cavity formedby thc inboard wheel half 12a. The brake assembly 20 includes a torque tube 30 mounted via a plurality of bolts 32 to a brake housing 3~ having brake actuating means 36 for applyin~ a braking pressure to a pressure plate 38, The pressure plate 38 transmits the braking pressure to a brake stac~ generally indicated by reference numeral 40 ~ 1~97~3 .~ 2 to e~fect braking o~' the wheel 12. Wheel braking action is accomplished by the brake stack 40 comprised o~ alter-nating brake ~isks 42 and ~'riction disks ~ either one o-f which may be keyed ~'or rotation with the wheel 12 or alternatively keyed -to be relatively stationary with the ,. torque tube 30. ~s illustrated in the drawing, the outer periphery ol' the rotatin~ members of the brake stack 40 are keyed to the inne:r periphery of the inboard wheel halL 12a while the inner periphery of' the stationary mem-bers of the stack 40 are keyed to the outer periphery o-P
the -torque tube 30. Thus,, the torque tube 30 plays a - primary role in the braking action and the design and construction o~' it is critical to the e~f'ectiveness of the brake sys-tem.
Conventionally, torque tubes of the prior art as illustrated in FIGURE 1 may comprise a one-piece forged or cast me-tal member 30 that is machined to close tolerances to provide the keyed interconnections for the stationary members Or the brake stack 40. Conventional torque tubes 30 ol' the prior art may also be characterized by an inte-gral backplate 30b that extends radially at an approximate angle o~' 90 degrees with respect to the cylindrical por-tion 30a ot' the tube and which operates to engage the brake stack 40 when a braking pressure is applied at the opposite end by -the actuating means 36 through the pressure plate 38. The prior art torque tube may further be characterized by a tubular portion 30a that carries -the keying elements 30c for engagement with the stationary members o~ the brake s-tack ~0 and these keying elements are conventionally machined in-to the outer peripheral sur-I'ace oL the torque -tube.
Prohlems associa-ted with conventionally forged or cast and machined torque tubes 30 involve the backplate 30b and' the drive key elements 30c. The backplate 30b may develop ~ractures due to the axial ~orce exerted on it and heat buildup during braking while the keys 30c su~fer ~ l~g7~3 `:

weal associated with braking action, In this circumstance, and because the backplate and keys are made as an inte-gral par-t ol' the torque tube, -the total torque tube must - be replace~ to put the brake assembly back into a safe and reliable operating condition, In this respect, the torque tube 30 is usually -the single mos-t expensive ele-ment of a typical brake assembly and therefore replace-ment o-t' it is a major maintenance operation and an ex-pensive proposition.
In view of' the above mentioned disadvantages of the presently used -torque tube, it is in one aspect of the present invention an objec-t to provide a torque tube assembly that eliminates replacement of the total torque tube when failure occurs to the backplate and/or drive key portions ol' the assembly, In another aspect of the invention i-t is an object to provide a torque tube that is more economical to manufac-ture and which does not require extensive machining operations and elaborate inspection techniques to meet rigid aircraft and/or industrial specifications, In another aspect of the invention it is an object -to provide a torque tube assembly that has separable drive keys which may be individually replaced when worn or defective keys are detected.
In still another aspect of the invention it is an ob,ject to provide a torque tube assembly having a sep-arable backplate that may be easily replaced when such backplate suffers fatigue failure and/or other defects, In another aspect of -the invention i-t is an object to provide a torque tube tha-t exhibits a longer service life than experienced with presently used one-piece torque -tubes and wherein -the operational integrity may be more easily tested, and which may be applied to brake assemblies having different diameters and numbers of drive keys.

9~

SUMMARY OF THE INVENTION

This invention provides in a brake assembly having an inboard end and an outboard end including a brake housing at the inboard end, an axle, a rotatable member on the axle at the outboard end, and a multi-disk brake stack of alternating rotating and ` stationary components to provide braking of the rotatable member when subjected to a pressure force on the brake stack, a sub-assembly for stationary mounting with respect to the brake housing to provide torque takeout, keying interconnections, and disk brake backup for the brake stack comprising in combination:
a cylindrically shaped torque tube mounted axially about the axle and having an inboard end as determ,ined by the brake housing and an outboard end as determined by the rotating member, said torque tube - having a plurality of spaced-apart slots in the tube about the periphery of each end wherein each slot at . the inboard end.is axially aligned with a respective slot in the outboard end; and a ~lurality of bar-shaped keys mounted axially on the torque tube in spanned relationship between one of said inboard and one of said outboard slots and engaged within said slots to provide keying interconnections for the stationary components of the brake stack and each said key having a .radial extension at the outboard end to provlde backup for the brake stack when said stack is subjected to a braking ~ressure force, said sub-assembly affixed to the brake housing by a plurality of bolts, each said bolt mounted in the brake housing and threadably engaged within the inboard end of a respective key.

7~3 .
DETAIL~I) r)1~lscRIpTIoN OF TIIR INVENTION
Re~erYing to FI~URES 2 thru 5 o-i the drawings, a -torque -tube assembly in accordance with -this invention is ~enerally indica-ted by re~erence numeral 100. The assembly 100 may be mounted about an aircra~t wheel axle (not shown~ having an axis Ax and orien-ted with respect to an inboard direction indicated by arrow 102 and an out-board dircction indicated by arrow 104. The assembly 100 generally comprises a torque tube member 50, a plurality o~ keys 60 axially aligned about the outer peripheral extent o~ the torque tube, and a brake backplate 70 mounted at the outboard end of the torque tube 50. The elements comprising torque tube 50, keys 60 and backplate 70 are individual and separable members o~ the assembly 100 and collectively replace the single torque tube element 30 illustratcd in FIGURE 1 o~ the drawings.
The torque tube 50 is an open-ended, wrought metal tube having a barrel portion 50a that terminates at the outboard end in a machine-~ormed -~lange 50b extending radially at an approxima-tc angle o~ 90 degrees with re-spect to thc Ax axis. At the inboard end the tube 50a terminates in a machine-~ormed restricted bore 50c that is adapted to moun-t on an axle assembly (not shown) in a conventional manner. The torque tube 50 is characterized by a plurality o~ slots 52 in spaced relationship about the inboard end o~ the tube and by an equal plurality o~
slots 54 in spaced relationship about the outboard end of the tubc 50. Each slo-t 52 at -the inboard end is axially aligned with a slot 54 at -the ou-tboard end o~ the tube.
Thc slots 52,54 are cut or machined into the torque tube 50 and each pair of slots 52,54 are o-~ a dimension such as to receive a drive key 60 in spanned relationship between them and in a substantially locking and anti-rotational arrangemen-t as will be more iully understood and appre-ciated hereina~ter. As mentioned, the torque tube 5p is a :
wrought me-tal tube and in this respect it may comprise a ligh-t gauge s-tock requiring a minimum amount of machining to shapc thc t,uhe to the iinal desixed configuration. It is anti~ipatcd, how~ve~Y, ~hat any hi~h strength metal may bc used Lor ~he torque tube including for example steel and titani-lm. Additional]y, the bore ot' the torque tube 50 may bc machined to Lurther decrease i-ts weight and in this resp~ct a center rib 50e may be provided to mount a supporting disc 51 within -the bore as a strengthening member. Thus, it will be appreciated by those persons skillcd in the brake arts that -the torque tube 50 of this invention is a much more simplified product requiring lower cos-t manufacturing techniques than the presently used one-piece torque tubes.
The torque tube 50 is adapted, by virtue of the slots 52,54, to carry a plurality of keying elements 60 about the ou-ter peripheral surl'ace o-f the barrel portion o-f the tube 50a. The keys 60 are forged or cast, bar-like ele-me~nts that may be made ol' solid bar stock steel or titanium and may be machined such as at 60c to reduce the weight thereof along the lengthwise extent of the bar.
The inboard end 60a o-f each key 60 is characterizec by a protrllsion 62 that depends and locks into the inboard slot 52. The outboard end 60b of each key 60 is charac-terized by a protrusion 64 that depends and locks intothe outboard slot 54. The slots 52,54 therefore provide an anti-rota-tional mounting for each of the keys 60. The keys 60 are -further a:Efixed to the torque tube 50 via bolts 66 that are mounted through holes 56 in the barrel portion 50a ol` the torque~ tube and threaded into matching threadcd holes 68 in the body o-f -the key. When all of the keying elemcnts 60 are mounted and affixed to the torque tube 50 the assembly is bolted -to -the stationary brake - housing 34 via bol-ts 69 that are threaded into each key 60 via threaded bores 60e provided in -the inboard end 60a.
In this manner torque--takeout of the brake assembly is provided by reasorl of the slots 52,5~, bolts 66, and bolts 69.
The keys 60 are fllrther characterized at their out-board extell-t by an e~xt;ension 60d tha-t extends radially outwarclly with L~espect to the Ax axis. As clearly illu-strated in FIGURES 2 and 5 of the drawings, the extension 60d is at an angle of approximately 90 degrees and is oriented within ~he torque tube slot 54 and aligned with the tube flange 50b. The drive key extensions 60d thus provide support :tor the backplate 70 by the number of keys mounted on the torque tube.
The~ backplate 70 is a circular disk having a bore 70a such that -the disk may be mounted on the assembly com-prising the torque tube 50 and keys 60. The backplate 70 has an overall diameter such as to provide sufficient support to a brake stack ("~0" in FIGURE 1) that may be moun-ted on the assembly. As clearly shown in the drawing, -the backplate 70 is supported at the outboard extent by the key extension 60d. The backplate 70 may also be pro-vided with a wear plate face 72 -that may be affixed to the backplate via any conventional fastening means such as for example rivets 7~.
While certain representative embodimen-ts and details have been shown Lor the purpose of illustrating the inven--tion, it will be apparent to those skilled in the art that various changes and modifications may be made therein with-out departing ~rom -the spirit or scope of the invention.

Claims (14)

WHAT IS CLAIMED IS:
1. In a brake assembly having an inboard end and an outboard end including a brake housing at the inboard end, an axle, a rotatable member on the axle at the out-board end, and a multi-disk brake stack of alternating rotating and stationary components to provide braking of the rotatable member when subjected to a pressure force on the brake stack, a sub-assembly for stationary mounting with respect to the brake housing to provide torque takeout, keying interconnections, and disk brake backup for the brake stack comprising in combination:
a cylindrically shaped torque tube mounted axially about the axle and having an inboard end as deter-mined by the brake housing and an outboard end as determined by the rotating member, said torque tube having a plurality of spaced-apart slots in the tube about the periphery of each end wherein each slot at the inboard end is axially aligned with a respective slot in the outboard end; and a plurality of bar-shaped keys mounted axially on the torque tube in spanned relationship between one of said inboard and one of said outboard slots and engaged within said slots to provide keying inter-connections for the stationary components of the brake stack and each said key having a radial exten-sion at the outboard end to provide backup for the brake stack when said stack is subjected to a brak-ing pressure force, said sub-assembly affixed to the brake housing by a plurality of bolts, each said bolt mounted in the brake housing and threadably engaged within the inboard end of a respective key.
2. The subassembly as set forth in claim 1 wherein each key is affixed to the torque tube via at least one bolt passing through the tube and threadably engaged within the body of the key.
3. The sub assembly as set forth in claim 1 further comprising a backplate disk mounted on the torque tube at the outboard end thereof and abutting the radial extensions of the keys to provide a backpressure plate for the brake stack when subjected to a braking pressure force.
4. The sub-assembly as set forth in claim 3 wherein the backplate disk is also in keying relationship with the keys on the torque tube.
5. the subassembly as set forth in claim 3 wherein the torque tube has a radially extending portion at the outboard end and the outboard end slots are cut through the extension, said radial extension of the tube and radial extensions of the keys providing a continuous radially extending backup for the backplate.
6. The sub-assembly as set forth in claim 1 wherein said torque tube has a radial extension within its bore to provide support to the tube in its mounting on the axle.
7. The sub-assembly as set forth in claim 1 wherein said keys are characterized by inboard and outboard exten-sions in the body of the key which depend into respective inboard and outboard slots, to seat into and engage the slots to provide torque takeout in the application of the brake.
8. The sub-assembly as set forth in claim 1 wherein the tube has a large diameter throughout the substantial portion of its length terminating through a radial portion in a smaller diameter at the inboard end thereof said inboard end slots being cut into the tube through the radial portion and into the large diameter portion.
9. An improved brake assembly having an inboard end and an outboard end including a brake housing at the inboard end, an axle, a rotatable member on the axle at the outboard end, a torque tube mounted about the axle, a multi-disk brake stack of alternating rotating and stationary components, said rotating components keyed for rotation with the rotatable member and the stationary components keyed to the torque tube to provide braking of the rotatable member when subjected to a pressure force on said brake stack, the improvement comprising:
a cylindrically shaped torque tube having an inboard end as determined by the brake housing and an outboard end as determined by the rotatable member and having a plurality of spaced-apart slots within the body of the tube and about its periphery at the inboard and outboard ends thereof, each said slot at the inboard end being axially aligned with a respective slot at the outbard end; and a plurality of bar-shaped separable keys mounted axially on the torque tube, each key in spanned relationship between one of said inboard and one of said outboard slots and engaged within the slots and affixed to the tube via at least one bolt at the approximate midsection of the tube and threadably engaged within the body of the key, each said key having a radial extension at the outboard end thereof to provide backup support for the brake stack when a braking pressure is applied to the inboard end of the stack and each said key having a threaded bore at the inboard end wherein the torque tube and keys are mounted to the brake housing by a plurality of bolts extending through the housing and received within a respective key.
10. The brake assembly as set forth in claim 9 wherein the torque tube is characterized by a radial extension at the outboard end thereof and said outboard slots are cut through said radial extension, the radial extension of the torque tube and the radial extension of the keys providing a continuous radially extending backup for the brake stack.
11. The brake assembly as set forth in claim 10 wherein a separable backplate disk is mounted on the torque tube, at the outboard end thereof, which disk abuts the radial extensions of the keys and torque tube.
12. The brake assembly as set forth in claim 9 wherein the torque tube is characterized by a large diameter through-out the substantial portion of its length terminating through a radial portion in a restricted diameter at the inboard end thereof, said inboard end slots being cut into the tube through the radial portion and into the large diameter portion.
13. The brake assembly as set forth in claim 12 wherein the torque tube is characterized by a radially extending rib within the bore of the tube to provide support of the tube in its mounting about the axle.
14. The brake assembly as set forth in claim 9 wherein each bar-shaped key is mounted on the torque tube via at least two bolts threaded into the body portion of the key at spaced positions along the length of the key and portions of the body of the key outside the influence of the bolts are machined to reduce the weight of the key.
CA000399624A 1981-06-08 1982-03-29 Configuration for a disk brake torque tube assembly having replaceable keys and backplate Expired CA1169783A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/271,343 US4383594A (en) 1981-06-08 1981-06-08 Configuration for a disk brake torque tube assembly having replaceable keys and backplate
US271,343 1981-06-08

Publications (1)

Publication Number Publication Date
CA1169783A true CA1169783A (en) 1984-06-26

Family

ID=23035172

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000399624A Expired CA1169783A (en) 1981-06-08 1982-03-29 Configuration for a disk brake torque tube assembly having replaceable keys and backplate

Country Status (6)

Country Link
US (1) US4383594A (en)
EP (1) EP0067113B1 (en)
JP (1) JPS57208328A (en)
BR (1) BR8202991A (en)
CA (1) CA1169783A (en)
DE (1) DE3269145D1 (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4878563A (en) * 1984-07-13 1989-11-07 The B.F. Goodrich Company Brake apparatus
GB2161560B (en) * 1984-07-13 1988-11-09 Goodrich Co B F Wheel and brake assembly
US4696376A (en) * 1986-04-30 1987-09-29 Loral Corporation Configuration for a disk brake torque tube
USRE36363E (en) * 1987-11-27 1999-11-02 Tilton Engineering Carbon to carbon friction clutch
US5186521A (en) * 1991-09-24 1993-02-16 Allied-Signal Inc. Wheel and drive key assembly
EP0662201B1 (en) * 1992-08-13 2002-12-11 Tilton Engineering, Inc. Carbon to carbon friction mechanism
US6109401A (en) * 1995-02-15 2000-08-29 Itt Manufacturing Enterprises Inc. Light-weight disc brake
US5862890A (en) * 1996-01-16 1999-01-26 Mcdonnell Douglas Corporation Restrained aircraft brake apparatus
US5931269A (en) * 1997-04-21 1999-08-03 Alliedsignal Inc. Aircraft wheel part with corrosion and wear resistance
US6752248B2 (en) 2001-09-04 2004-06-22 Honeywell International Inc. Multi-disc brake structural asymmetry
GB2438633B (en) * 2006-05-31 2010-12-01 Tisics Ltd Reinforced splines and their manufacture
US8776955B2 (en) * 2007-02-02 2014-07-15 Warner Electric Technology Llc Liquid cooled brake with support columns
FR2937949B1 (en) * 2008-11-04 2011-05-27 Messier Bugatti WHEEL BARREL AND WHEEL SPECIALLY ADAPTED
US9850968B2 (en) * 2014-04-29 2017-12-26 Goodrich Corporation Torque bar and methods for making
US11644071B2 (en) 2019-07-08 2023-05-09 Honeywell International Inc. Rotor drive key assembly
BR112023022988A2 (en) * 2021-05-04 2024-01-30 Meggitt Aircraft Braking Systems Corp TORQUE TUBE

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1556427A (en) * 1924-09-24 1925-10-06 Brownlipe Gear Company Clutch consturction having toothed fiber disks
GB579172A (en) * 1942-07-04 1946-07-25 Bendix Aviat Corp Improvements in or relating to disk brakes
US2559885A (en) * 1947-11-28 1951-07-10 Goodrich Co B F Disk brake
GB651876A (en) * 1948-04-07 1951-04-11 Dunlop Rubber Co Improvements in disc brake and wheel assemblies
US2764261A (en) * 1953-04-03 1956-09-25 James H Bridges Brake disc retainer
GB751626A (en) * 1953-06-05 1956-07-04 Siam Improvements in disc brakes for wheels
GB764097A (en) * 1953-09-28 1956-12-19 Bendix Aviat Corp Improvements in or relating to wheel and brake assemblies
US3061050A (en) * 1958-09-03 1962-10-30 Goodrich Co B F Wheel and brake assembly
US3138032A (en) * 1961-09-25 1964-06-23 Emerson Electric Co Axially adjustable drive mechanism
US3237731A (en) * 1964-01-23 1966-03-01 Bendix Corp Disc brake rotor construction
US3250349A (en) * 1964-03-20 1966-05-10 American Brake Shoe Co Disc brake
US3436106A (en) * 1965-12-17 1969-04-01 Emerson Electric Co Key drive for sliding hubs
FR1523402A (en) * 1967-03-22 1968-05-03 Hispano Suiza Lallemant Soc Improvements to multiple disc brakes, especially for aircraft wheels
US3727477A (en) * 1971-05-04 1973-04-17 M Murphy Power transmission
GB1402534A (en) * 1971-07-27 1975-08-13 Dunlop Ltd Wheel assemblies
GB1402535A (en) * 1971-07-27 1975-08-13 Dunlop Ltd Wheel assemblies
US3754624A (en) * 1971-09-17 1973-08-28 Bendix Corp Flexible key for disc brake
GB1443709A (en) * 1972-12-19 1976-07-21 Dunlop Ltd Disc brakes
US3977631A (en) * 1975-06-04 1976-08-31 The Boeing Company Aircraft wheel drive apparatus and method
SU566987A1 (en) * 1976-02-13 1977-07-30 Предприятие П/Я М-5287 Key joint of a shaft with a bush

Also Published As

Publication number Publication date
US4383594A (en) 1983-05-17
EP0067113A2 (en) 1982-12-15
DE3269145D1 (en) 1986-03-27
EP0067113A3 (en) 1983-04-13
EP0067113B1 (en) 1986-02-19
JPS57208328A (en) 1982-12-21
BR8202991A (en) 1983-05-03

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